TABLE OF CONTENTS
1. GENERAL PROVISIONS
1.1. HELICOPTER REQUIREMENTS
1.2. HELICOPTER CERTIFICATION
1.3. MATERIALS AND PRODUCTION TECHNIQUE
1.4. SUPERVISION AND TESTING METHODS
1.5. HELICOPTER PROOFING
1.6. STENCILLING AND INSCRIPTIONS ON THE HELICOPTER
2. A BRIEF DESCRIPTION OF THE HELICOPTER
2.1 CONSTRUCTIONS AND LAYOUT DIAGRAM
2.2. HELICOPTER TYPE AND DESIGNATION
2.3. ENGINE TYPE AND QUANTITY
2.4. DEVELOPER AND MODEL
2.5. CREW PERSONNEL AND HELICOPTER’S TRANSPORTING CAPABILITIES
2.6. OUTER COATING
3. MAIN FEATURES
3.1. ESTIMATED WEIGHTS
З.2. REGULATION CURVES
3.3. CENTERING CHARACTERISTICS
3.4. FLIGHT CHARACTERISTICS
3.5. GEOMETRICAL DIMENSIONS
3.6. ENGINE INFORMATION
3.7. GEOMETRICAL ADJECTIVES OF THE ROTORS
3.8. ALTITUDE RANGES, OPERATING TEMPERATURE RANGES, AND WEATHER CONDITIONS
3.9. LIFETIME
4. BRIEF DESCRIPTION OF THE HELICOPTER’S CONSTRUCTION
4.1. GENERAL PROVISIONS
4.2. MATERIALS USED
4.3. FRAMEWORK
4.4. COCKPIT
4.5. TAIL BOOM
4.6. UNDERCARRIAGE
4.7. ROTOR
4.8. ANTI-TORQUE ROTOR
5. PROPULSION AND TRANSMISSION
5.1. GENERAL INFORMATON
5.2. ENGINE
5.3. TRANSMISSION
5.4. NOISE LEVEL
6. CONTROLLING SYSTEM
6.1. GENERAL PROVISIONS
6.2. WOBBLE PLATE
6.3. CONTROLS
7. POWER-SUPPLY SYSTEM
7.1. GENERAL PROVISIONS
7.2. 12V AND 27V DIRECT-CURRENT SYSTEM
7.3. 36V THREE-PHASE ALTERNATE CURRENT SYSTEM
8 FUEL SYSTEM
8.1. GENERAL PROVISIONS
9. HEATING AND EVAPORATION SYSTEM
9.1. GENERAL CHARACTERISTICS
10. GENERAL PROCESS TECHNOLOGY CHARACTERISTICS
GENERAL PROVISIONS
1.1.HELICOPTER REQUIREMENTS The AK1-3 helicopter complies with the requirements of AP 27 Normal Category Rotary Wing Flight Suitability Norms, which comply with the FAA flight suitability standards for civil aircraft (FAR-27).
1.2. HELICOPTER CERTIFICATION
AK1-3 helicopter is registered for certification with the State Aircraft Department of Ukraine.
АК1-3 complies with the requirements of the certification basis for the helicopter developed according to:
- AP-27 normal category flight suitability norms;
- noise abatement requirements as laid down in Chapter 3 of Appendix 16 of the International Civil Aircraft Convention (Chicago 1944), volume 1, Aviation Noise, 3rd edition 1933; and the requirements of Part 3 of Aviation Rules (AP-36).
1.3. MATERIALS AND PRODUCTION TECHNIQUE
In producing the helicopter, the materials and techniques applied comply with the existing aviation standards and other reference documents.
1.4. SUPERVISION AND TESTING METHODS The supervision and testing during manufacturing are carried out according to the existing reference documents.
1.5. HELICOPTER PROOFING The helicopter's inner and outer surface proofing is carried out according to the existing reference documents.
1.6. STENCILLING AND INSCRIPTIONS ON THE HELICOPTER
All inscriptions on the helicopter’s outer surface, stenciling and inscriptions in the cockpit and on the controls are in Russian. Under the customer’s wishes, stenciling and inscriptions can be done in a foreign language.A BRIEF DESCRIPTION OF THE HELICOPTER
2.1 CONSTRUCTIONS AND LAY-OUT DIAGRAM
2.1.1. The AK1-3 helicopter (Fig. 2.1) is a fabricated structure with a 3-bladed rotor and a 2-bladed anti-torque rotor.
2.2. HELICOPTER TYPE AND DESIGNATION
2.2.1. The helicopter falls into the normal category of light aircraft, and is designated to fulfill the following tasks:
- Patrolling (power lines, canals, pipelines, highways, hard-to-reach border regions);
- Agriculture (pollination, spraying, sowing, animal watch);
- Forest and wild animal protection;
- Advertising;
- Searching;
- Aerial inspection (aerial photography, geological and fishing exploration);
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本文鏈接地址：Ultra light Helicopter AK1-3
